CN104908945A - Saucer-shaped aircraft - Google Patents
Saucer-shaped aircraft Download PDFInfo
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- CN104908945A CN104908945A CN201410094617.4A CN201410094617A CN104908945A CN 104908945 A CN104908945 A CN 104908945A CN 201410094617 A CN201410094617 A CN 201410094617A CN 104908945 A CN104908945 A CN 104908945A
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Abstract
The invention relates to a saucer-shaped aircraft which is designed to mainly solve the problem that existing aircraft is great in oil consumption and the like. The aircraft comprises an upper shell and a rotary wing, wherein the upper shell is internally provided with a rotor and a stator, an upper cabin is connected with an upper central shaft; a commutator is installed on the anode and cathode electric brushes on the upper shell are contacted with the commutator; the anode and cathode of a storage battery in the upper cabin are respectively connected with an upper bearing and an upper big bearing, the upper big bearing is sleeved with a lead and is connected with the electric brush of the other pole; a middle cabin is flexibly connected with an upper positioning plate, a rod of an upper hydraulic cylinder is movably connected with the upper positioning plate, a side cabin is arranged outside the middle cabin, an operating table and a hydraulic pump are arranged in the middle cabin, the middle cabin is flexibly connected with a lower positioning plate, and the rod of a lower hydraulic cylinder is movably connected with a lower positioning plate; a rotary wing is further arranged on the lower shell; the lower cabin is connected with a lower central shaft which is provided with a commutator, and the lower shell is internally provided with a rotor and a stator. A landing foot is arranged at the bottom end of the rod of a landing hydraulic cylinder; a storage battery is arranged in the lower cabin, and the cathode and anode of the storage battery are respectively connected with a lower bearing and a lower big bearing. The saucer-shaped aircraft has the advantage of no oil consumption.
Description
Technical field:
The present invention relates to a kind of disc-shaped flying craft.
Background technology:
Existing aircraft is fuel mainly with fuel oil, and shortcoming is that noise is large, and oil consumption is many, contaminated environment.Also having with electricity is the aircraft of power, but the electrical motor that they use be all stator outside, rotor, interior, does not have load space in electrical motor.About existing copter engine room accounts for the half of total weight.
Summary of the invention:
It is little that technical matters to be solved by this invention is to provide a kind of noise, pollution-free, and landing is steady, and outside, stator, interior, has the disc-shaped flying craft of load space to rotor in electrical motor.
Above-mentioned purpose is achieved in that it comprises cylindrical shape upper casing, cylindrical shape upper casing top is fixed with egg end, cylindrical shape upper casing outer wall is fixed with several rotors, rotor passes top cover sidepiece and is interconnected and fixed with top cover, cylindrical shape upper casing inwall there are some fan leafs, cylindrical shape upper casing is provided with several heat radiation pores, cylindrical shape upper casing internal fixtion is by the rotor be made up of two semicircle magnet, several curved I shape ferrosilicon of silicon steel plate stacking are had inside two semicircle magnet, several curved I shape ferrosilicon form a circle, winding is wound around along the axis of cylinder in the space (i.e. wire casing) formed between the I-shaped of each curved I shape ferrosilicon, each curved I shape ferrosilicon and winding composition stator, air gap is had between stator and rotor, cylindrical shape upper-deck cabin is equipped with in the central authorities of the circle that each curved I shape ferrosilicon forms, cylindrical shape upper-deck cabin outer wall and each curved I shape ferrosilicon inwall are connected and fixed, the upper cover of cylindrical shape upper-deck cabin central connection with the lower end of hollow upper center shaft seals, the central authorities of cylindrical shape upper casing and the overcoat of head bearing are connected and fixed, insulating barrier is had between the central authorities of cylindrical shape upper casing and the overcoat of head bearing, the inner sleeve of head bearing is sleeved on center shaft top, commutator is sleeved on the below that center shaft top is positioned at head bearing, insulating barrier is provided with between upper center shaft and commutator and head bearing, insulating barrier is had between the inner sleeve of head bearing and upper center shaft, the lower edge of cylindrical shape upper casing is connected and fixed with the cover insulation of upper large bearing, upper large bearing inner sleeve to be sleeved on annular arrangement on position plate, go up on large bearing inner sleeve and annular arrangement and have insulating barrier between position plate, along being connected and fixed with position plate on annular arrangement under cylindrical shape upper-deck cabin, the inwall of cylindrical shape upper casing center of top is fixed with positive and negative electrode brush, and the positive and negative electrode brush on cylindrical shape upper casing center of top inwall contacts with the commutator be fixed on upper center shaft, and this commutator and the connection mode of winding are that closed loop series excitation type is connected,
Upper-deck cabin is built with storage battery, in upper-deck cabin, a pole of storage battery has wire to be upwards connected with head bearing inner sleeve along upper center shaft inwall, because bearing is conductor, so the energising of head bearing overcoat, connect with a pole brush, in upper-deck cabin, another pole of storage battery has wire to be connected with the upper large bearing inner sleeve that upper position plate is set with, and its overcoat is energized, and upper large bearing outside has wire be upwards connected with another pole brush at cylindrical shape upper casing top along cylindrical shape upper casing inwall;
The upper edge of cylindrical shape middle deck is flexible coupling with position plate on annular arrangement, cylindrical shape middle deck outer wall top is circumferentially fixed with hydraulic actuating cylinder on several uniformly, the cylinder bar of each upper hydraulic actuating cylinder is lived with position plate on annular arrangement and is connected, cabin, side is had outside cylindrical shape middle deck, the edge up and down in cabin, side is connected and fixed with the edge up and down of middle deck bulkhead respectively, operator's station and Hydraulic Pump is provided with in cylindrical shape middle deck, all master cocies and source switch are all located on operator's station, hydraulic pipe is had to be connected between Hydraulic Pump with each hydraulic actuating cylinder, along being flexible coupling with position plate under circle under cylindrical shape middle deck, cylindrical shape middle deck outer wall bottom is circumferentially fixed with several lower hydraulic actuating cylinders uniformly, each lower hydraulic cylinder bar is lived with position plate under circle and is connected, circular lower position plate has the hatch door passed through for personnel and goods, on the bulkhead in cabin, side, Kai You looks at window,
Cylindrical shape lower casing outer wall is fixed with several rotors, cylindrical shape lower casing outer wall is fixed with arc outer cover, described rotor passes outer cover and is interconnected and fixed with outer cover, and cylindrical shape lower casing inwall has some fan leafs, and cylindrical shape lower casing is provided with several heat radiation pores, under cylindrical shape, the upper cover central authorities in cabin are connected and fixed with hollow lower center shaft lower end, the top of lower center shaft is set with commutator, lower have insulating barrier between center shaft and commutator, under cylindrical shape cabin on cover and be provided with hatch door, the upper end of lower center shaft is fixedly connected with the central authorities of lower position plate, lower center shaft top is sleeved in lower bearing, between position plate and commutator, insulating barrier is had between lower bearing inner sleeve and lower center shaft, insulating barrier is had between lower bearing and commutator, cylindrical shape lower casing internal fixtion is by the rotor be made up of two semicircle magnet, several curved I shape ferrosilicon of silicon steel plate stacking are had inside two semicircle magnet, several curved I shape ferrosilicon form a circle, winding is wound around along the axis of cylinder in the space (i.e. wire casing) formed between the I-shaped of each curved I shape ferrosilicon, each curved I shape ferrosilicon and winding composition stator, air gap is had between stator and rotor, under each curved I shape ferrosilicon inwall and cylindrical shape, wall is connected and fixed out of my cabin, the upper edge of cylindrical shape lower casing is connected and fixed with the overcoat of lower large bearing, the inner sleeve of lower large bearing is sleeved on lower position plate, insulating barrier is had between lower large bearing and cylindrical shape lower casing and lower position plate, the lower edge of cylindrical shape lower casing is connected and fixed with the cover insulation of base bearing, base bearing inner sleeve is sleeved on circular lower ceiling board, insulating barrier is had between ceiling board under base bearing inner sleeve and circle, under cylindrical shape, the lower edge in cabin is connected and fixed with ceiling board under circle, circular lower ceiling board is equipped with several landing hydraulic actuating cylinders, landing hydraulic cylinder bar down, there is landing pin each cylinder bar bottom, each landing hydraulic actuating cylinder has hydraulic oil pipe to be connected with the Hydraulic Pump in middle deck through lower center shaft, circular lower ceiling board is provided with hatch door, comes in and goes out for personnel's goods,
Also storage battery is housed in lower cabin, the brush of a pole is fixed on the little extension arm of lower bearing overcoat, the brush of another pole is fixed on the large extension arm on lower large bearing outside, this both positive and negative polarity brush contacts with the commutator be fixed on lower center shaft, one pole of storage battery has wire to be connected with lower bearing inner sleeve after lower center shaft outer wall is upward through the insulating barrier between commutator and lower center shaft, lower bearing overcoat is energized, be fixed on the brush energising on the little extension arm of lower bearing overcoat, another pole of storage battery has wire to hold large bearing inner sleeve and be connected with lower position plate overlaps, overcoat is energized, be fixed on the brush energising on the large extension arm of lower large bearing outside, the little extension arm put outside the large extension arm on large bearing outside and lower bearing is descended to be connected and fixed, insulating barrier is had between large extension arm and little extension arm,
Rotor on cylindrical shape upper casing outer wall is contrary with the rotor wing rotation direction on cylindrical shape lower casing outer wall.
During flight, heading is controlled with the hydraulic actuating cylinder on annular arrangement cylinder brackets, such as, to fly to the right, then make the cylinder bar on the right of the hydraulic cylinder bar on the left side on upper cylinder brackets and lower hydraulic actuating cylinder stretch out simultaneously, the cylinder bar of other hydraulic actuating cylinder stretches out along with shift ratio simultaneously, and upper and lower wing is tilted to the right.During landing, the landing hydraulic cylinder works of bottom, cabin under cylindrical shape, cylinder bar stretches out downwards.
Advantage of the present invention is: not fuel oil, and pollution-free, noise is little, rises and falls steadily, and lightweight, and load carrying ability is large, and outside, stator, interior, has load space in electrical motor to rotor.
Accompanying drawing illustrates:
Fig. 1 is structural representation of the present invention;
Fig. 2 is A-A view of Fig. 1.
Detailed description of the invention:
With reference to Fig. 1, 2, it comprises cylindrical shape upper casing 1, cylindrical shape upper casing top is fixed with egg end 2, cylindrical shape upper casing outer wall is fixed with several rotors 3, rotor passes top cover sidepiece and is interconnected and fixed with top cover, cylindrical shape upper casing inwall there are some fan leafs 4, cylindrical shape upper casing is provided with several heat radiation pores, cylindrical shape upper casing internal fixtion is by the rotor 5 be made up of two semicircle magnet, several curved I shape ferrosilicon 6 of silicon steel plate stacking are had inside two semicircle magnet, several curved I shape ferrosilicon form a circle, winding 7 is wound around along the axis of cylinder in the space (i.e. wire casing) formed between the I-shaped of each curved I shape ferrosilicon, each curved I shape ferrosilicon and winding composition stator, air gap is had between stator and rotor, cylindrical shape upper-deck cabin 8 is equipped with in the central authorities of the circle that each curved I shape ferrosilicon forms, cylindrical shape upper-deck cabin outer wall and each curved I shape ferrosilicon inwall are connected and fixed, the upper cover of cylindrical shape upper-deck cabin central connection with the lower end of hollow upper center shaft 9 seals, the central authorities of cylindrical shape upper casing and the overcoat of head bearing 10 are connected and fixed, insulating barrier is had between the central authorities of cylindrical shape upper casing and the overcoat of head bearing, the inner sleeve of head bearing is sleeved on center shaft top, commutator 11 is sleeved on the below that center shaft top is positioned at head bearing, insulating barrier is provided with between upper center shaft and commutator and head bearing, insulating barrier is had between the inner sleeve of head bearing and upper center shaft, the lower edge of cylindrical shape upper casing is connected and fixed with the cover insulation of upper large bearing 12, upper large bearing inner sleeve to be sleeved on annular arrangement on position plate 13, go up on large bearing inner sleeve and annular arrangement and have insulating barrier between position plate, along being connected and fixed with position plate on annular arrangement under cylindrical shape upper-deck cabin, the inwall of cylindrical shape upper casing center of top is fixed with positive and negative electrode brush 14, and the positive and negative electrode brush on cylindrical shape upper casing center of top inwall contacts with the commutator be fixed on upper center shaft, and this commutator and the connection mode of winding are that closed loop series excitation type is connected,
Upper-deck cabin is built with storage battery, in upper-deck cabin, a pole of storage battery has wire to be upwards connected with head bearing inner sleeve along upper center shaft inwall, because bearing is conductor, so the energising of head bearing overcoat, connect with a pole brush, in upper-deck cabin, another pole of storage battery has wire to be connected with the upper large bearing inner sleeve that upper position plate is set with, and its overcoat is energized, and upper large bearing outside has wire be upwards connected with another pole brush at cylindrical shape upper casing top along cylindrical shape upper casing inwall;
The upper edge of cylindrical shape middle deck 15 is flexible coupling with position plate on annular arrangement 13, cylindrical shape middle deck outer wall top is circumferentially fixed with hydraulic actuating cylinder 16 on several uniformly, the cylinder bar of each upper hydraulic actuating cylinder is lived with position plate on annular arrangement and is connected, cabin, side 17 is had outside cylindrical shape middle deck, the edge up and down in cabin, side is connected and fixed with the edge up and down of middle deck bulkhead respectively, operator's station 18 and Hydraulic Pump 19 is provided with in cylindrical shape middle deck, all master cocies and source switch are all located on operator's station, hydraulic pipe is had to be connected between Hydraulic Pump with each hydraulic actuating cylinder, along being flexible coupling with position plate under circle 20 under cylindrical shape middle deck, cylindrical shape middle deck outer wall bottom is circumferentially fixed with several lower hydraulic actuating cylinders 21 uniformly, each lower hydraulic cylinder bar is lived with position plate under circle and is connected, circular lower position plate has the hatch door passed through for personnel and goods, on the bulkhead in cabin, side, Kai You looks at window 22,
Cylindrical shape lower casing 23 outer wall is fixed with several rotors 3, cylindrical shape lower casing outer wall is fixed with arc outer cover 24, described rotor passes outer cover and is interconnected and fixed with outer cover, and cylindrical shape lower casing inwall has some fan leafs, and cylindrical shape lower casing is provided with several heat radiation pores, under cylindrical shape, the upper cover central authorities in cabin 25 are connected and fixed with hollow lower center shaft 26 lower end, the top of lower center shaft is set with commutator, lower have insulating barrier between center shaft and commutator, under cylindrical shape cabin on cover and be provided with hatch door, the upper end of lower center shaft is fixedly connected with the central authorities of lower position plate 20, lower center shaft top is sleeved in lower bearing 27, between position plate and commutator, insulating barrier is had between lower bearing inner sleeve and lower center shaft, insulating barrier is had between lower bearing and commutator, cylindrical shape lower casing 23 internal fixtion is by the rotor 5 be made up of two semicircle magnet, several curved I shape ferrosilicon 6 of silicon steel plate stacking are had inside two semicircle magnet, several curved I shape ferrosilicon form a circle, winding 7 is wound around along the axis of cylinder in the space (i.e. wire casing) formed between the I-shaped of each curved I shape ferrosilicon, each curved I shape ferrosilicon and winding composition stator, air gap is had between stator and rotor, under each curved I shape ferrosilicon inwall and cylindrical shape, cabin 25 outer wall is connected and fixed, the upper edge of cylindrical shape lower casing 23 is connected and fixed with the overcoat of lower large bearing 28, the inner sleeve of lower large bearing is sleeved on lower position plate, insulating barrier is had between lower large bearing and cylindrical shape lower casing and lower position plate, the lower edge of cylindrical shape lower casing is connected and fixed with the cover insulation of base bearing 29, base bearing inner sleeve is sleeved on circular lower ceiling board 30, insulating barrier is had between ceiling board under base bearing inner sleeve and circle, under cylindrical shape, the lower edge in cabin is connected and fixed with ceiling board under circle, circular lower ceiling board is equipped with several landing hydraulic actuating cylinders 31, landing hydraulic cylinder bar down, there is landing pin 32 each cylinder bar bottom, each landing hydraulic actuating cylinder has hydraulic oil pipe to be connected with the Hydraulic Pump in middle deck through lower center shaft, circular lower ceiling board is provided with hatch door, comes in and goes out for personnel's goods,
Also storage battery is housed in lower cabin, the brush of a pole is fixed on the little extension arm 34 of lower bearing overcoat, the brush of another pole is fixed on the large extension arm 33 on lower large bearing outside, this both positive and negative polarity brush contacts with the commutator be fixed on lower center shaft, one pole of storage battery has wire to be connected with lower bearing inner sleeve after lower center shaft outer wall is upward through the insulating barrier between commutator and lower center shaft, lower bearing overcoat is energized, be fixed on the brush energising on the little extension arm of lower bearing overcoat, another pole of storage battery has wire to hold large bearing inner sleeve and be connected with lower position plate overlaps, overcoat is energized, be fixed on the brush energising on the large extension arm of lower large bearing outside, the little extension arm put outside the large extension arm on large bearing outside and lower bearing is descended to be connected and fixed, insulating barrier is had between large extension arm and little extension arm,
Rotor on cylindrical shape upper casing outer wall is contrary with the rotor wing rotation direction on cylindrical shape lower casing outer wall.
Claims (1)
1. a disc-shaped flying craft, comprise cylindrical shape upper casing (1), it is characterized in that: cylindrical shape upper casing top is fixed with egg end (2), cylindrical shape upper casing outer wall is fixed with several rotors (3), rotor passes top cover sidepiece and is interconnected and fixed with top cover, cylindrical shape upper casing inwall there are some fan leafs (4), cylindrical shape upper casing is provided with several heat radiation pores, cylindrical shape upper casing internal fixtion is by the rotor be made up of two semicircle magnet (5), several curved I shape ferrosilicon (6) of silicon steel plate stacking are had inside two semicircle magnet, several curved I shape ferrosilicon form a circle, winding (7) is wound around along the axis of cylinder in the space formed between the I-shaped of each curved I shape ferrosilicon, each curved I shape ferrosilicon and winding composition stator, air gap is had between stator and rotor, cylindrical shape upper-deck cabin (8) is equipped with in the central authorities of the circle that each curved I shape ferrosilicon forms, cylindrical shape upper-deck cabin outer wall and each curved I shape ferrosilicon inwall are connected and fixed, the upper cover of cylindrical shape upper-deck cabin central connection with the lower end of hollow upper center shaft (9) seals, the overcoat of the central authorities of cylindrical shape upper casing and head bearing (10) is connected and fixed, insulating barrier is had between the central authorities of cylindrical shape upper casing and the overcoat of head bearing, the inner sleeve of head bearing is sleeved on center shaft top, commutator (11) is sleeved on the below that center shaft top is positioned at head bearing, insulating barrier is provided with between upper center shaft and commutator and head bearing, insulating barrier is had between the inner sleeve of head bearing and upper center shaft, the lower edge of cylindrical shape upper casing is connected and fixed with the cover insulation of upper large bearing (12), upper large bearing inner sleeve is sleeved on position plate on annular arrangement (13), go up on large bearing inner sleeve and annular arrangement and have insulating barrier between position plate, along being connected and fixed with position plate on annular arrangement under cylindrical shape upper-deck cabin, the inwall of cylindrical shape upper casing center of top is fixed with positive and negative electrode brush (14), positive and negative electrode brush on cylindrical shape upper casing center of top inwall contacts with the commutator be fixed on upper center shaft, and this commutator and the connection mode of winding are that closed loop series excitation type is connected,
Upper-deck cabin is built with storage battery, in upper-deck cabin, a pole of storage battery has wire to be upwards connected with head bearing inner sleeve along upper center shaft inwall, in upper-deck cabin, another pole of storage battery has wire to be connected with the upper large bearing inner sleeve that upper position plate is set with, and upper large bearing outside has wire be upwards connected with another pole brush at cylindrical shape upper casing top along cylindrical shape upper casing inwall;
The upper edge of cylindrical shape middle deck (15) is flexible coupling with position plate on annular arrangement (13), cylindrical shape middle deck outer wall top is circumferentially fixed with hydraulic actuating cylinder on several (16) uniformly, the cylinder bar of each upper hydraulic actuating cylinder is lived with position plate on annular arrangement and is connected, cabin, side (17) is had outside cylindrical shape middle deck, the edge up and down in cabin, side is connected and fixed with the edge up and down of middle deck bulkhead respectively, operator's station (18) and Hydraulic Pump (19) is provided with in cylindrical shape middle deck, all master cocies and source switch are all located on operator's station, hydraulic pipe is had to be connected between Hydraulic Pump with each hydraulic actuating cylinder, along being flexible coupling with position plate under circle (20) under cylindrical shape middle deck, cylindrical shape middle deck outer wall bottom is circumferentially fixed with several lower hydraulic actuating cylinders (21) uniformly, each lower hydraulic cylinder bar is lived with position plate under circle and is connected, circular lower position plate has the hatch door passed through for personnel and goods, on the bulkhead in cabin, side, Kai You looks at window (22),
Cylindrical shape lower casing (23) outer wall is fixed with several rotors (3), cylindrical shape lower casing outer wall is fixed with arc outer cover (24), described rotor passes outer cover and is interconnected and fixed with outer cover, cylindrical shape lower casing inwall has some fan leafs, and cylindrical shape lower casing is provided with several heat radiation pores, under cylindrical shape, the upper cover central authorities of cabin (25) are connected and fixed with hollow lower center shaft (26) lower end, the top of lower center shaft is set with commutator, lower have insulating barrier between center shaft and commutator, under cylindrical shape cabin on cover and be provided with hatch door, the upper end of lower center shaft is fixedly connected with the central authorities of lower position plate (20), lower center shaft top is sleeved in lower bearing (27), between position plate and commutator, insulating barrier is had between lower bearing inner sleeve and lower center shaft, insulating barrier is had between lower bearing and commutator, cylindrical shape lower casing (23) internal fixtion is by the rotor be made up of two semicircle magnet (5), several curved I shape ferrosilicon (6) of silicon steel plate stacking are had inside two semicircle magnet, several curved I shape ferrosilicon form a circle, winding (7) is wound around along the axis of cylinder in the space formed between the I-shaped of each curved I shape ferrosilicon, each curved I shape ferrosilicon and winding composition stator, air gap is had between stator and rotor, under each curved I shape ferrosilicon inwall and cylindrical shape, cabin (25) outer wall is connected and fixed, the upper edge of cylindrical shape lower casing (23) is connected and fixed with the overcoat of lower large bearing (28), the inner sleeve of lower large bearing is sleeved on lower position plate, insulating barrier is had between lower large bearing and cylindrical shape lower casing and lower position plate, the lower edge of cylindrical shape lower casing is connected and fixed with the cover insulation of base bearing (29), base bearing inner sleeve is sleeved on circular lower ceiling board (30), insulating barrier is had between ceiling board under base bearing inner sleeve and circle, under cylindrical shape, the lower edge in cabin is connected and fixed with ceiling board under circle, circular lower ceiling board is equipped with several landing hydraulic actuating cylinders (31), landing hydraulic cylinder bar down, there is landing pin (32) each cylinder bar bottom, each landing hydraulic actuating cylinder has hydraulic oil pipe to be connected with the Hydraulic Pump in middle deck through lower center shaft, and circular lower ceiling board is provided with hatch door,
Also storage battery is housed in lower cabin, the brush of a pole is fixed on the little extension arm (34) of lower bearing overcoat, the brush of another pole is fixed on the large extension arm (33) on lower large bearing outside, this just, negative pole brush contacts with the commutator be fixed on lower center shaft, one pole of storage battery has wire to be connected with lower bearing inner sleeve after lower center shaft outer wall is upward through the insulating barrier between commutator and lower center shaft, another pole of storage battery has wire to hold large bearing inner sleeve and be connected with lower position plate overlaps, the little extension arm put outside the large extension arm on large bearing outside and lower bearing is descended to be connected and fixed, insulating barrier is had between large extension arm and little extension arm,
Rotor on cylindrical shape upper casing outer wall is contrary with the rotor wing rotation direction on cylindrical shape lower casing outer wall.
Priority Applications (1)
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CN201410094617.4A CN104908945A (en) | 2014-03-15 | 2014-03-15 | Saucer-shaped aircraft |
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CN201410094617.4A CN104908945A (en) | 2014-03-15 | 2014-03-15 | Saucer-shaped aircraft |
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CN201410094617.4A Pending CN104908945A (en) | 2014-03-15 | 2014-03-15 | Saucer-shaped aircraft |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105752330A (en) * | 2016-02-19 | 2016-07-13 | 张红艳 | Disk-like aircraft capable of adjusting flying attitude |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3276723A (en) * | 1964-02-28 | 1966-10-04 | Astro Kinetics Corp | Vtol flight unit |
US4165848A (en) * | 1976-08-09 | 1979-08-28 | Alfredo Bizzarri | Rotary thrust device including axially elongated rotor rotatable in casting having elongated fluid intake and discharge slots |
CN102390533A (en) * | 2011-09-22 | 2012-03-28 | 厦门大学 | Saucer-shaped aircraft |
CN102642621A (en) * | 2012-05-22 | 2012-08-22 | 秦长余 | Flight vehicle |
CN202593857U (en) * | 2012-02-10 | 2012-12-12 | 杜云鹏飞 | Solar electromagnetic power saucer-shaped aircraft |
CN203780799U (en) * | 2014-03-15 | 2014-08-20 | 秦长余 | Saucer-shaped aircraft |
-
2014
- 2014-03-15 CN CN201410094617.4A patent/CN104908945A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3276723A (en) * | 1964-02-28 | 1966-10-04 | Astro Kinetics Corp | Vtol flight unit |
US4165848A (en) * | 1976-08-09 | 1979-08-28 | Alfredo Bizzarri | Rotary thrust device including axially elongated rotor rotatable in casting having elongated fluid intake and discharge slots |
CN102390533A (en) * | 2011-09-22 | 2012-03-28 | 厦门大学 | Saucer-shaped aircraft |
CN202593857U (en) * | 2012-02-10 | 2012-12-12 | 杜云鹏飞 | Solar electromagnetic power saucer-shaped aircraft |
CN102642621A (en) * | 2012-05-22 | 2012-08-22 | 秦长余 | Flight vehicle |
CN203780799U (en) * | 2014-03-15 | 2014-08-20 | 秦长余 | Saucer-shaped aircraft |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105752330A (en) * | 2016-02-19 | 2016-07-13 | 张红艳 | Disk-like aircraft capable of adjusting flying attitude |
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Application publication date: 20150916 |